The present invention relates generally to turbines. More specifically, to attaching ceramic matrix composites (CMC) in gas turbines to metal components with a bolt.
Generally, ceramic matrix composite turbine components require attachment to adjoining metallic hardware and/or metallic surfaces. Two disadvantages associated with attaching a CMC to metallic hardware are the wear of the metallic hardware by the hard, abrasive ceramic material surface, and the lack of load distribution in the CMC. Additionally, differences between the coefficients of thermal expansion between the metal and ceramic matrix composite make attaching metal and ceramic matrix composites challenging.
Therefore, a ceramic matrix composite (CMC) component and a method of attaching a metal component to a CMC component that do not suffer from the above drawbacks is desirable in the art.
According to an exemplary embodiment of the present disclosure, a ceramic matrix composite and a metal attachment configuration is provided. The ceramic matrix composite and a metal attachment configuration includes a metal plate having a metal plate aperture. The ceramic matrix composite and a metal attachment configuration includes a ceramic matrix composite plate adjacent the metal plate and having a ceramic matrix composite plate aperture aligned with the metal plate aperture. The ceramic matrix composite and a metal attachment configuration includes a spacer adjacent to the ceramic matrix composite, the spacer having a spacer aperture aligned with the metal plate aperture and the ceramic matrix composite aperture. The ceramic matrix composite and a metal attachment configuration includes a metal bolt having a first end and a second end, the second end operable to fit into the aligned spacer aperture, ceramic matrix composite plate aperture, and metal aperture to attach the spacer, the ceramic matrix composite plate and the metal plate. The ceramic matrix composite and a metal attachment configuration includes a nut adjacent to the metal plate and operable to receive the second end of the bolt. The spacer allows the metal plate having a high coefficient of thermal expansion to be attached to the ceramic matrix composite plate having a low coefficient of thermal expansion.
According to another exemplary embodiment of the present disclosure, a ceramic matrix composite and metal attachment configuration is provided. The ceramic matrix composite and metal attachment configuration includes a metal plate having a metal plate aperture. The ceramic matrix composite and metal attachment configuration includes a ceramic matrix composite plate adjacent the metal plate and including a ceramic matrix composite plate aperture aligned with the metal plate aperture. The ceramic matrix composite and metal attachment configuration includes a metal bolt having a first end, a second end, and a channel running therethrough. The second end of bolt is operable to fit into the aligned ceramic matrix composite plate aperture, and metal aperture to attach the ceramic matrix composite plate and the metal plate. The ceramic matrix composite and metal attachment configuration includes a nut adjacent to the metal plate and operable to receive the second end of the bolt. The channel of the metal bolt minimizes growth of the bolt relative to the ceramic matrix composite plates due to mismatch of coefficient of thermal expansion between the metal bolt and the metal plate and the ceramic matrix composite plate.
Other features and advantages of the present invention will be apparent from the following more detailed description of the preferred embodiment, taken in conjunction with the accompanying drawings which illustrate, by way of example, the principles of the invention.
Wherever possible, the same reference numbers will be used throughout the drawings to represent the same parts.
Provided are ceramic matrix composite and metal attachment configurations to attach ceramic matrix composites to metal components having different coefficients of thermal expansions.
One advantage of an embodiment of the present disclosure includes providing an attachment configuration for attaching CMC components that have a low thermal expansion coefficient (αCMC) to metal component that have a high thermal expansion coefficient (αmetal) relative to CMC components.
According to one embodiment a ceramic matrix composite and metal attachment configuration including a metal plate and a ceramic matrix composite plate is provided. For example,
According to one embodiment, spacer may be a metal and have a coefficient of thermal expansion that is the same or different from the metal bolt or metal plate. For example, in
According to one embodiment, ceramic matrix composite and metal attachment configuration may include metal plate, ceramic matrix composite plate, spacer, metal bolt, and nut. For example, as shown in
According to one embodiment ceramic matrix composite and metal attachment configuration may include a metal plate, a ceramic matrix composite plate, a metal bolt, a nut, and a spring. For example, in
According to one embodiment, a ceramic matrix composite and metal attachment configuration is provided. For example as shown in
According to one embodiment, a zero CMC thickness joint may be obtained. For example, as shown in
While the invention has been described with reference to a preferred embodiment, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiment disclosed as the best mode contemplated for carrying out this invention, but that the invention will include all embodiments falling within the scope of the appended claims.
This patent application claims the benefit of U.S. Provisional Patent Application Ser. No. 61/666,826 filed on Jun. 30, 2012, and entitled “CERAMIC MATRIX COMPOSITE AND METAL ATTACHMENT CONFIGURATIONS,” the disclosure of which is incorporated by reference as if fully rewritten herein.
Number | Date | Country | |
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61666826 | Jun 2012 | US |